U.S. patent number 3,775,039 [Application Number 05/217,097] was granted by the patent office on 1973-11-27 for burners for liquid or gaseous fuels.
This patent grant is currently assigned to Enterprise Generale De Chauffage Industriel Pillard Freres et Cie. Invention is credited to Marcel T. Pillard.
United States Patent |
3,775,039 |
Pillard |
November 27, 1973 |
BURNERS FOR LIQUID OR GASEOUS FUELS
Abstract
This invention relates to a burner for liquid or gaseous fuels
composed of hree coaxial ducts, the intermediate duct and the outer
duct defining an annular space for distributing the
combustion-supporting air, which burner comprises fins placed in
said annular space, behind the nozzle of the burner, and means
forming a perforated screen, placed in said intermediate space,
downstream of the fins, so that an eddy of burning fluid is formed
about the nozzle of the burner.
Inventors: |
Pillard; Marcel T. (Marseille,
FR) |
Assignee: |
Enterprise Generale De Chauffage
Industriel Pillard Freres et Cie (Marseille,
FR)
|
Family
ID: |
9071278 |
Appl.
No.: |
05/217,097 |
Filed: |
January 12, 1972 |
Foreign Application Priority Data
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Jan 22, 1971 [FR] |
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7103504 |
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Current U.S.
Class: |
431/350; 239/406;
431/183 |
Current CPC
Class: |
F23D
11/00 (20130101); F23D 17/002 (20130101) |
Current International
Class: |
F23D
17/00 (20060101); F23D 11/00 (20060101); F23m
009/08 () |
Field of
Search: |
;431/182,183,185,350,351
;239/405,406 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Favors; Edward G.
Claims
What is claimed is:
1. Burner of liquid or gaseous fuels composed of three coaxial
cylindrical ducts: a central duct, of small diameter, for
distributing the fuel, terminated by a nozzle forming the nozzle of
the burner; an intermediate duct, of slightly larger diameter, for
distributing the primary combustion-supporting air, terminated by a
nozzle at its end adjacent said first-mentioned nozzle and an outer
duct, of larger diameter than said intermediate duct, defining with
said intermediate duct an annular space in which the secondary
combustion-supporting air circulates, said burner comprising in
addition fins which occupy the larger part of said annular space,
and which are recessed with respect to said end of said
intermediate duct and means forming a perforated screen disposed on
the periphery of said intermediate duct, downstream of said fins,
so that there is formed, under the shelter of said screen and
around said end of said intermediate duct, an eddy of burning fluid
which extends in part upstread of said first-mentioned nozzle.
2. Burner as claimed in claim 1, in which said screen means are
constituted by a disc, placed on the periphery of said intermediate
duct, the outer diameter of which is substantially equal to the one
half the diameter of said outer duct, which disc comprises channels
of small diameter passing right through it, said channels supplying
the eddy of burning fluid with combustion air without blowing it
out.
3. Burner as claimed in claim 2, in which said disc is constituted
by a hub carrying said fins on its periphery, through which are
pierced channels parallel to the axis of the burner.
4. Burner as claimed in claim 2 in which said disc is constituted
by a hub carrying said fins on its periphery, through which are
pierced channels inclined with respect to the axis and converging
forwardly.
5. Burner as claimed in claim 1, in which the fins are curved,
their upstream edge is parallel to the axis and their downstream
edge forms with the axis of the burner an angle which decreases
from the hub to the periphery of the fins where the downstream edge
is parallel to the axis.
6. Burner as claimed in claim 1, in which the cylindrical and
coaxial air deflectors are disposed between said fins.
7. Burner as claimed in claim 2, in which said fins are fixed to
the inner wall of said outer duct and are independent of said disc
which is fixed to the periphery of said intermediate duct and said
intermediate and outer ducts are movable longitudinally with
respect to one another so that the relative position of the disc
and the fins may be modified.
8. Burner as claimed in claim 3 in which said outer conduit
comprises, to the rear, a lateral combustion air inlet opening,
which burner comprises, in addition, a cylindrical air valve
sliding about said outer duct in order to regulate the surface of
said opening and a longitudinally sectioned air deflector located
inside said outer duct, downstream of said air inlet opening, which
deflector is integral with said sliding valve.
9. Burner as claimed in claim 8, wherein said deflector is
connected to said valve by its upstream end which is normally
connected to the wall of said valve about the end of said valve
which defines the air inlet opening and the downstream end of said
deflector is parallel to the inner wall of said outer duct against
which it slides.
10. Burner as claimed in claim 9, comprising, in addition, a second
fixed deflector located inside said annular space, in the rear part
thereof, the section of which is substantially parallel to that of
the movable deflector and a third fixed truncated deflector placed
upstream of said hub, the diameter of the upstream end of which is
slightly larger than the outer diameter of said intermediate tube
and the diameter of the downstream end of which is substantially
equal to the outer diameter of said hub.
Description
The present invention relates to burners for liquid or gaseous
fuels.
It is known that the burners of liquid fuels provided in industrial
boilers or furnaces generally comprise a central duct, or injection
nozzle, for distributing the fuel under pressure, terminating at
its end, on the furnace side, by at atomising nozzle. This nozzle
projects the droplets of liquid fuel in divergent directions, whose
envelope is substantially a cone of revolution about the axis of
the burner.
In the case of gaseous fuels, it is substantially the same case,
and only the way in which the fuel is projected in order to
constitute the jets which are mixed with the combustion-supporting
air, varies.
The combustion-supporting air is distributed in a cylindrical duct
of larger diameter, coaxial with the injection nozzle.
The air may be divided into two parts, the primary air distributed
in an intermediate duct and the secondary air distributed in an
outer duct. The secondary air may or may not be animated by a
rotary movement about the axis of the burner by means of fins
disposed in the secondary air duct. About the nozzle of the burner,
eddies of air tend to be formed which are animated by a high speed
of rotation, these air eddies being located between the cone of
projection of fuel and the central layers of combustion-supporting
air. The centrifugal force due to this speed tends to project
droplets of liquid fuel laterally or to drive part of the gaseous
fuel outwardly which pass through the layers of
combustion-supporting air without completely burning. This results
in a poor combustion which produces smoke and soot.
The author of the present invention has noted that these eddies
could be beneficial on condition that they are ignited. Experience
has shown that the clinging of the flame to the nozzle of the
burner and the quality of the combustion and ignition are clearly
bettwe when a toric eddy is created about the nozzle of the burner,
extending in part to the rear of the nozzle of the burner, formed
of a mixture of fuel and combustion-supporting air taken from the
two currents which enframe said eddy and when this eddy is supplied
with combustion-supporting air in order to maintain it burning
without the supply of combustion-supporting air being too intense
and risking eliminating said eddy by blowing it out.
It is therefore an object of the invention to create an eddy of
burning fluid around the nozzle of the burner.
This aim is attained by disposing fins in the secondary combustion
air duct which are recessed with respect to the nozzle of the
burner and by placing, downstream of said fins a perforated screen
under whose shelter a zone of depression is formed in which an eddy
of burning fluid is created.
The result of the formation of this eddy is a better combustion
enabling the excess of air to be reduced to a maximum, this
diminishing the smoke and reducing the risks of formation of
sulphuric acid from the usual fuels containing sulphur.
In a particular embodiment, the burner comprises three coaxial
ducts : a central duct for distributing the fuel, an intermediate
duct for distributing the primary combustion-supporting air and an
outer duct for distributing the secondary combustion-supporting air
and the fins are fixed to the periphery of a hub surrounding the
intermediate duct, the diameter of which is substantially equal to
half the diameter of the outer conduit, which hub is pierced with
channels of small diameter which transverse is right through in
order to supply the eddy with combustion air.
These channels may be parallel to the axis or converging towards
the front. In this case, it is the hub which fulfills the function
of screen.
The diameter of the perforations or of the channels feeding the
eddy with combustion air must be small and determined with accuracy
in order not to destroy the depression behind the screen.
The fins are preferably curved, their upstream edge being parallel
to the axis and the downsteam edge forming with the axis an angle
which decreases from the centre up to the periphery where it
becomes parallel to the axis.
Thanks to this arrangement, the layers of combustion-supporting air
located near the centre have a higher tangential speed, this
causing turbulences and facilitating the formation of the eddy.
Cylindrical deflectors, coaxial with the burner, may be placed
between the fins. These deflectors divide the secondary
combustion-supporting air into separate layers, this reducing the
interactions between layers which cause disturbances in the flow of
the secondary combustion-supporting air, which would risk
destroying the eddy of burning fluid.
In a particular embodiment of the invention, the fins are fixed to
the inner wall of the outer duct and the perforated disc forming
the screen is fixed to the intermediate duct, substantially in the
same plane perpendicular to the axis. The outer duct and the
intermediate duct are movable with respect to each other so that
the relative position of the fins and the screen can be slightly
modified, by trial and error, in order to look for the position
which gives the eddy the most extensive and most stable
position.
In combination with the perforated screen, under whose shelter the
eddy is formed, air deflectors are preferably used, placed upstream
of the fins, which are sectioned longitudinally in order to pipe
the air upstream of the fins and to quieten the flow, whilst
avoiding the parasitic turbulences.
In the frequent case of the burner comprising a valve sliding
opposite the air inlet located in the lateral wall of the outer
duct in order to regulate the surfaces of this opening and the
outflow of combustion-supporting air, one of the deflectors,
located inside the outer duct, is integral with said valve on which
is is perpendicularly connected all around said opening.
The burner according to the invention differs from the known
turbulence devices, for example : -- the deflector disc provided
with a central aperture -- the conical flame deflectors -- the
flame boxes.
These known devices have a different aim. They create a zone of
turbulence about the flame or inside the flame but none of them
enables an eddy of burning fluid to be obtained, located in part to
the rear of the nozzle of the burner. The means used are also
different, none of these devices comprising, to the rear of the
nozzle of the burner, a screen under whose shelter a zone of
depression is formed.
Devices exist which comprise, in the duct distributing
combustion-supporting air, a "rosette" with fins fixed to a hub.
However, this hub fulfills the exclusive mechanical role of support
for the fins. It is not large enough to form a screen and it does
not comprise channels passing right through.
The accompanying drawings illustrate, by way of example,
embodiments of devices in accordance with the invention which are
described hereinafter.
FIG. 1 is a longitudinal section of a device according to the
invention.
FIG. 2 is a transverse section along III--III of FIG. 1.
FIG. 3 is a longitudinal section through a rosette equipping
another device according to the invention.
FIG. 4 is a longitudinal section of another device according to the
invention.
FIG. 5 is a longitudinal section through another device comprising
a gaseous fuel distribution.
FIG. 6 is a longitudinal section through a device comprising
combustion air deflectors upstream of the rosette.
Referring now to the drawings, FIG. 1 shows a duct 1 for
distributing fuel, terminated by a nozzle 2. The duct 1 is disposed
along axis x--x' of a tube 3 terminated by a conical nozzle 4. On
the outer periphery of the tube 3 and recessed with respect to the
nozzle, there is disposed a large solid cylindrical hub 5 carrying
on its periphery radial fins 6 forming a rosette whose axis is
merged with the axis x--x'. The whole is placed inside a
cylindrical air distributor duct 7 which may or may not be widened
at its front end. The fins 6 occupy a large part of the space
between the hub 5 and the duct 7.
The fuel is projected in diverging directions, whose envelope is
constituted by the cone of revolution 8. The combustion-supporting
air arrives in duct 7 at a longitudinal velocity in the direction
of arrows A. The fins 6 are inclined on axis x--x' so that on
leaving the fins, the combustion-supporting air is animated by a
speed having a transverse component which is constant or variable
according to the radius. The air layers, on leaving the rosette,
form concentric hyperboloids.
A zone of depression is thus constituted under shelter of the hub
which forms a screen. In this zone there is formed an eddy 10
revolving about the axis x--x'. This eddy causes particles of fuel
or incompletely burnt gases to be driven upstream. The combustion
continues in the eddy which is ignited due to the air driven
peripherally or by injection through the hub.
FIG. 2 shows the device of FIG. 1 in transverse section. The fins
of this divice have an entry surface whose tangential plane is
substantially parallel to the axis x--x' whilst the downstream edge
is inclined on the axis x--x'. The inclination of the downsteam
edge decreased from the centre to the periphery so that the
rotation of the layers of air near the centre is stronger than that
of the layers located on the periphery.
As a variant, the fins may be flat or with curvilinear section and
of width decreasing from the centre to the periphery in order that,
as before, the central layers of air have a greater speed of
rotation, this favouring the formation of the central eddy of the
flame and of the toric eddy.
In order to supply the eddy of burning fluid with combustion air,
small holes 15 which are parallel to the axis x--x' or inclined
with respect thereto in one or two directions, may be pierced
through the hub 5.
The zone of the eddy is particularly favourable for placing therein
the devices for igniting the flame, such as electrodes generating
electric sparks or pilot light.
FIG. 3 shows another embodiment in which like elements are
designated by the same reference numerals. This device differs from
the preceding one in that it comprises, between the fins 6 of the
rosette, circular deflectors 11a, 11b, for piping the air and
separating the layers of combustion-supporting air into several
elementary hyperboloids.
FIG. 4 shows another embodiment in longitudinal section.
The elements similar to those of the preceding Figures are
designated by the same reference numbers. This FIG. shows the whole
of the device including the valve for the inlet of
combustion-supporting air which penetrates into the cylindrical
conduit 7 in the direction of arrows 12, through a peripheral
opening.
The outflow of combustion-supporting air may be regulated by
adjusting the width of the opening by means of a sliding valve 13
actuated by the manoeuvring key 14.
In this embodiment, the fins 6, which constitute the rosette, are
fixed to the duct 7 by means of the radial centering fins 16 and
are independent of the hub 5 which is fixed to the duct 3. This
arrangement enables the relative position of the nozzle of the
burner to be varied with respect to the rosette in order to find
the one which corresponds to the best combustion.
FIG. 5 shows an embodiment comprising a burner that may be a mixed
burner with liquid or gaseous fuel or a solely gas burner. The
arrangement of the rosette and the hub remains identical to that of
the previous Figure. The combustion air duct 7 comprises a double
wall 7a, 7b and the intermediate space serves as a duct for
distributing fuel gas which is injected through apertures 17 which
may or may not be provided with elongated nozzles placed in front
of the rosette 6 either perpendicularly to the wall, inclined
forwardly, or inclined rearwardly in order that part of the jets of
gas supplies the toric eddy 10 in order for it to remain burning,
as in the previous cases.
FIG. 6 shows another embodiment, like elements being designated by
like reference numerals. The combustion air penetrates radially in
the direction of arrows 12 into duct 7. The sliding valve 13
enables the outflow of air to be regulated. Longitudinally
sectioned deflectors pipe the combustion air from the radial
direction to the rosette 6, so that the flow of air remains
laminar. These deflectors are composed of a surface 18 revolving
about axis x--x', which is fixed to the rear wall of the device and
of another surface 19 revolving about x--x', fixed to the sliding
valve.
The deflector possibly comprises, in addition, a cone of revolution
20 upstream of the hub 5, which pipes the streams of air up to the
fins of the rosette.
The longitudinal sections of the surfaces 18 and 19 are obviously
studied to eliminate the formation of any parasitic eddy along the
walls.
The combination of the deflectors 18, 19 and possibly 20 with a
rosette 6 and a hub 5 forming a screen and clearly recessed with
respect to the nozzle of the burner results in the formation of a
very regular eddy 10 of burning fluid, with a very stable
flame.
* * * * *